N131QS

Service difficulty reports not matched to an aircraft · 16

They name N131QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N131QS' AND registry_match IS NULL
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DXTA2013061805420Starter Gen · failedAFTER STARTING LEFT ENGINE, AN ELECTRICAL ODOR WAS NOTICED IN THE COCKPIT. TROUBLESHOT AND FOUND LT ENGINE STARTER/GENERATOR TO HAVE BURNED SMELL FOLLOWING ENGINE START. ALSO, EXCESSIVE AMOUNT OF BLACK SOOT ON LOWER ENGINE AFT OF STARTER/GEN EXHAUST. CONFIRJun 18, 2013 · N131QS · Raythn 400ARAYTHEON · Air Distribution SystemSDR DXTA2013032205330Pressure Switch · failedJUST PRIOR TO LEVELING OFF AT FL 270, RT FUEL TRANSFER PRESSURE LOW ANNUNCIATOR BEGAN CYCLING ON AND OFF ERRATICALLY. FUSELAGE TANK ALMOST EMPTY, AND TRANSFER PUMP SWITCHES WERE IN AUTO. WITHIN ONE MINUTE, THE LT SIDE DID, AS WELL. ACCOMPLISHED ABNORMAL CHEMar 22, 2013 · N131QS · Beech 400A · Aircraft Fuel Distribution SystemSDR DXTA2012123105219Line · disconnectedAPPROX TWO HOURS AFTER FUELING AND 1.5 HOURS OF CLOSED CABIN, FUEL ODOR WAS NOTICED ENTERING CABIN. INSPECTING LUGGAGE COMPARTMENT REVEALED EVEN STRONGER ODOR, ESPECIALLY COMING OUT OF INSPECTION PANELS. GAINED ACCESS TO AFT FUSELAGE FUEL TANK. INSPECTED AFTDec 28, 2012 · N131QS · Beech 400A · Fuel StorageSDR DXTA2012122605214Unknown · odorAPPROX 2 HOURS AFTER FUELING AND 1.5 HRS OF CLOSED CABIN, FUEL SMELL WAS NOTICED ENTERING CABIN. INSPECTING LUGGAGE COMPARTMENT REVEALED EVEN STRONGER SMELL, ESPECIALLY COMING OUT OF INSPECTION PANELS. INSPECTED AFT BAGGAGE AREA FOR FUEL LEAKS. NO DEFECTS NODec 25, 2012 · N131QS · Beech 400A · Air Distribution SystemSDR DXTA2012062205009Landing Gear · malfunctionedON APPROACH, EXPERIENCED AN UNSAFE RED LIGHT IN THE GEAR HANDLE, ACCOMPANIED WITH THE AURAL GEAR-WARNING HORN AFTER SELECTING FLAPS FROM 20 TO 30 DEGREES. AFTER ABORTING THE APPROACH TO COMPLETE RELEVANT CHECKLIST, RETRACTED THE FLAPS, WHICH SILENCED HORN, BJun 21, 2012 · N131QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DXTA2011080904698Brake Assy · malfunctionedLT BRAKE PEDAL ON COPILOTS SIDE BLEEDS OFF PRESSURE WHEN BRAKES ARE APPLIED WHILE THE RT PEDAL REMAINED SOLID WITH BRAKE PRESSURE. KEPT HAVING TO PUMP THE LT BRAKE PEDAL IN ORDER TO BUILD UP PRESSURE ON THE PEDAL, BUT THIS ONLY LASTED MOMENTARILY AND THE PRESAug 9, 2011 · N131QS · Raythn 400ARAYTHEON · Landing Gear Brake SystemSDR DXTA2008122003414Circuit Card · faultyON DESCENT INTO PDK THE RUDDER BOOST FAILED. AUTO PILOT DISCONNECTED AND COPILOTS FD FAILED. COMPLETED RUDDER BOOST FAIL CHECK LIST WITH NO CHANGE. TROUBLESHOT SYS, FOUND NR 2 FCC CARD FAULTY. REMOVED AND REPLACED NR 2 FCC CARD WITH CUSTOMER SUPPLIED OVERHAUDec 20, 2008 · N131QS · Raythn 400ARAYTHEON · Navigation System WiringSDR DXTA2008122203414Autopilot Sys · malfunctionedON DESCENT THE RUDDER BOOST FAILED. AUTO PILOT DISCONNECTED & COPILOTS FD FAILED.Dec 20, 2008 · N131QS · Raythn 400ARAYTHEON · Autopilot SystemSDR DXTA200803114Pressure Switch · failedRT BOOST PUMP LIGHT ILLUMINATED WHILE ACFT WAS IN CRUISE AT FL 350. CREW DID NOT NOTICE IF RT FUEL LOW PRESS FAILURE LIGHT ON ANNUNICATOR PANEL ILLUMINATED MOMENTARILY OR NOT. PERFORMED CHECKLIST FOR JET PUMP FAILURE. INSTALLED A NEW LOW FUEL PRESSURE SWITCH. Jun 12, 2008 · N131QS · Raythn 400ARAYTHEON · Fuel Pressure IndicatorSDR DXTA20082900Unknown · odorELECTRICAL ODOR IN LAVATORY. REMOVED ALL PANELS IN LAV AREA. COULD NOT DUPLICATE ODOR. INSPECTED ALL WIRES, PC BOARDS TERMINALS ETC. FOR SIGNS OF DAMAGE. NO DEFECTS NOTED. SUPPLIED GROUND POWER TO AIRCRAFT THROUGHOUT ENTIRE INSPECTION PROCESS. SUPPLIED GROFeb 26, 2008 · N131QS · Beech 400A · Air Distribution SystemSDR DXTA200802835Indicator · inoperativeON TAKEOFF LT OIL TEMP WENT TO 0, ABORTED TAKEOFF. SWAPPED GAUGES FROM RT TO LT, STARTED ENGINES, DID FIND OIL TEMP NEEDLE DID NOT RISE TAPPED ON GAUGE AND IT CAME UP. SWAPPED GAUGES TO THE ORIGINAL POSITION, RAN ENGINES AGAIN PROBLEM STILL FOLLOWED. REPLACEDFeb 4, 2008 · N131QS · Beech 400A · Engine Oil TemperatureSDR DXTA200802786Switch · out of adjustINITIAL SELECTION OF FLAPS 10DEG AT 200KIAS FLAP ASYM CAUTION LIGHT CAME ON. TROUBLESHOT, ADJUSTED LT AND RT FLAP FOLLOW UP SWITCHES, AND LT FLAP POSITION TRANSMITTER, ALSO ADJUSTED RT FLAP FOLLOW UP SWITCH LINK AREA AND CHECKED FLAP TRAVEL ANGLES. ALL CHECKEJan 22, 2008 · N131QS · Beech 400A · Trailing Edge Flap Control SystemSDR DXTA200702408Switch · looseON APPROACH TO FTY THE LEFT MAIN LANDING GEAR LIGHT WOULD NOT ILLUMINATE. WE RECYCLED THE GEAR TWO TIMES, AND ALSO VERIFIED THE LIGHT BULB WORKED WITH THE IND LIGHTS TEST. WE ALSO USED THE ALTERNATE GEAR EXTENSION PROCEDURE AND THE LIGHT WOULD NOT ILLUMIATE. Aug 15, 2007 · N131QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200702023Landing Gear · inoperativeCOULD NOT GET RT MAIN GEAR LIGHT USED ALTERNATE GEAR EXTENSION. TROUBLESHOT SYSTEM AND FOUND RT MLG DOWNLOCK SWITCH TO BE SHORTED AND NOT REPORTING POSITION. REMOVED AND INSTALLED NEW SWITCH IAW HAWKER 400XP MM 32-60-00. OPS CHECK OF SYSTEM SHOWS NORMAL OPERAMar 15, 2007 · N131QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DXTA200701976Speed Brake · slowON APPROACH HAD A UNCOMMANDED TURN TO THE RT WITH SPEED BRAKES EXTENDED. AIRCRAFT WAS AT APPROACH SPEED. CHECKED LEFT AND RIGHT SPOILER CABLE TENSIONS FOUND NORMAL AT 82 FOUND IAW HAWKER 400XP M.M. CH 27-60-00 CHART 201. FOUND LEFT SIDE SPEEDBRAKE EXTENDING Feb 28, 2007 · N131QS · Beech 400A · Drag Control SystemSDR DXTA200601563Downlock Switch · faultyON GEAR EXTENSION HAD INDICATION OF LT AND RT MAINS ONLY NO NOSE INDICATION. PERFORMED THE LANDING GEAR NOT DOWN AND LOCKED CHECKLIST AFTER CYCLING THE GEAR AGAIN. LANDED NORMALLY. NOSE GEAR INDICATED GREEN AFTER LANDING. REPLACED NOSE GEAR DOWN LOCK SWITCH WAug 19, 2006 · N131QS · Beech 400A · Landing Gear Position and Warning
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